Composite ac-to-dc power converter with boosting capabilities

ABSTRACT

A boosting AC-to-DC converter may include a main rectifier, first and second auxiliary rectifiers, and an autotransformer. The autotransformer may include a plurality of winding assemblies each having a primary terminal connected to an AC power source, a main secondary terminal connected to the main rectifier, a first auxiliary secondary terminal connected to the first auxiliary rectifier, and a second auxiliary secondary terminal connected to the second auxiliary rectifier. Impedance between the primary terminal of each of the winding assemblies and the main rectifier is less than impedance between the primary terminal of each of the winding assemblies and either the first auxiliary rectifier or the second auxiliary rectifier. Impedance between the primary terminal of each of the first winding assemblies and the first auxiliary rectifier is different from impedance between the primary terminal of each of the winding assemblies and the second auxiliary rectifier.

BACKGROUND OF THE INVENTION

The present invention generally relates to AC-to-DC converters and moreparticularly to passive AC-to-DC converters with voltage boostingcapability.

AC-to-DC converters play a significant role in the modernaerospace/military industry. This is particularly true in the area ofmore electric architecture (MEA) for aircraft and spacecraft. Powerquality is a major concern for MEA aircraft because of the large numberof electric power systems and equipment installed on the same bus. Thepower quality of these systems and equipment has stringent requirementsto ensure that all power supplies/utilization equipment functiontogether properly.

The term “composite AC-to-DC converter” has been coined to distinguish aconverter using two or more conversion methods in parallel. The conceptfor a composite AC-to-DC converter originated as a further improvementtowards smaller size, lower weight, and higher efficiency.

While composite AC-to-DC converters present a large step towardperformance improvement they have not incorporated efficient boostingcapabilities. They typically provide rectification of a three phase115-Vac system resulting in a typical output voltage value of 270 Vdc.There are many applications where the output voltage is desired to bemuch higher for a better performance of a consecutive powerconditioning. Typical values used in some power distribution systems are540 Vdc, +/−270 Vdc and 610 Vdc. That means that it would be desirablefor a composite AC-to-DC converter, used in a three phase 115-Vacsystem, to produce output voltage about two times higher at itsrectified output. In other words, it would be desirable to providevoltage boosting capability in a composite AC-to-DC converter.

It would be desirable to achieve such voltage boosting passively whileintroducing only minimal harmonic distortions to input AC currents.Typically, lower frequency harmonic distortions may be reduced byemploying AC-to-DC converters with high pulse configurations. Forexample, when conversion of three phase AC power is performed with a24-pulse converter, harmonic distortions of input power may bemaintained at a reasonably low level. Of course, a 24-pulse convertermust have a higher number of transformer windings than a 12-pulse or18-pulse converter. Consequently, 24-pulse converters are typicallyheavier, larger and more expensive than 12-pulse or 18-pulse converters.Such sizes and weights may be evaluated objectively by considering andexpression W/VA: where W is DC power in watts; and VA is the rating of atransformer expressed in volt-amperes. For a typical 18-pulse converterwith a 1:2 boosting capability, W/VA may be about 0.5.

Additionally, it would be desirable to achieve passive voltage boostingemploying an autotransformer, as compared to an activesemiconductor-based boosting circuit. In the context of aerospaceapplications inherent reliability of a passive system as compared to anactive system is an important consideration.

Within an autotransformer of a composite AC-to-DC converter, interiorwinding turn ratios are responsible for its voltage boost factor.However a typical autotransformer's conversion ratio (ACR) will begin todecrease when used for voltage boosting. The main cause of a decreasingACR in a boost topology can be viewed as the autotransformer windingvolts*amperes (VA) sum is going up while the autotransformer outputpower is remaining constant. A high ACR is desirable in anautotransformer used in an aerospace vehicle because such anautotransformer may be constructed with smaller windings and with lessweight than an autotransformer having a low ACR.

As can be seen, there is a need for a passive composite AC-to-DCconverter with voltage boosting capability. More particularly, there isa need for such a converter that may produce voltage boosting passivelywith an autotransformer which may operate with a high ACR and withminimal harmonic distortion of input voltage.

SUMMARY OF THE INVENTION

In one aspect of the present invention, a multi-phase AC-to-DC convertermay comprise: a main rectifier; a first auxiliary rectifier; a secondauxiliary rectifier; and an autotransformer coupled with the mainrectifier, the first auxiliary rectifier and the second auxiliaryrectifier, the autotransformer including; a first winding assemblyincluding: a primary terminal coupled with an AC power source, a mainsecondary terminal coupled with the main rectifier, a first auxiliarysecondary terminal coupled with the first auxiliary rectifier, and asecond auxiliary secondary terminal coupled with the second auxiliaryrectifier, wherein operational impedance between the primary terminaland the main secondary terminal is less than operational impedancebetween the primary terminal and either the first auxiliary secondaryterminal or the second auxiliary secondary terminal, and whereinoperational impedance between the primary terminal and the firstauxiliary secondary terminal is different from operational impedancebetween the primary terminal and the second auxiliary secondaryterminal; a second winding assembly including, a primary terminalcoupled with the AC power source, a main secondary terminal coupled withthe main rectifier, a first auxiliary secondary terminal coupled withthe first auxiliary rectifier, and a second auxiliary secondary terminalcoupled with the second auxiliary rectifier, wherein operationalimpedance between the primary terminal and the main secondary terminalis less than operational impedance between the primary terminal andeither the first auxiliary secondary terminal or the second auxiliarysecondary terminal and wherein operational impedance between the primaryterminal and the first auxiliary secondary terminal is different fromoperational impedance between the primary terminal and the secondauxiliary secondary terminal; and a third winding assembly including, aprimary terminal coupled with the AC power source, a main secondaryterminal coupled with the main rectifier, a first auxiliary secondaryterminal coupled with the first auxiliary rectifier, and a secondauxiliary secondary terminal coupled with the second auxiliaryrectifier, wherein operational impedance between the primary terminaland the main secondary terminal is less than operational impedancebetween the primary terminal of the third winding assembly and eitherthe first auxiliary secondary terminal or the second auxiliary secondaryterminal and wherein operational impedance between the primary terminaland the first auxiliary secondary terminal is different from operationalimpedance between the primary terminal and the second auxiliarysecondary terminal.

In another aspect of the present invention, an autotransformer for usein an AC to DC converter may comprise: a first winding assembly thatincludes a plurality of winding segments and at least one tap; a secondwinding assembly that includes a plurality of winding segments and atleast one tap; a third winding assembly that includes a plurality ofwinding segments and at least one tap; wherein at least one windingsegment of the first winding assembly is coupled with the at least onetap of the second winding assembly, wherein at least one winding segmentof the second winding assembly is coupled with the at least one tap ofthe third winding assembly, and wherein at least one winding segment ofthe third winding assembly is coupled with the at least one tap of thefirst winding assembly.

These and other features, aspects and advantages of the presentinvention will become better understood with reference to the followingdrawings, description and claims.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a schematic diagram of an AC-to-DC power converter inaccordance with an embodiment of the invention;

FIG. 2 is a vector-format schematic diagram of an autotransformer of theconverter of FIG. 1 in accordance with an embodiment of the invention;

FIG. 3 is a conventional schematic diagram of the autotransformer of theconverter of FIG. 1 in accordance with an embodiment of the invention;

FIG. 4 is a schematic diagram of an AC-to-DC power converter inaccordance with a second embodiment of the invention; and

FIG. 5 is a schematic diagram of an AC-to-DC power converter inaccordance with a third embodiment of the invention.

DETAILED DESCRIPTION OF THE INVENTION

The following detailed description is of the best currently contemplatedmodes of carrying out exemplary embodiments of the invention. Thedescription is not to be taken in a limiting sense, but is made merelyfor the purpose of illustrating the general principles of the invention,since the scope of the invention is best defined by the appended claims.

Various inventive features are described below that can each be usedindependently of one another or in combination with other features.

Broadly, embodiments of the present invention generally provide passivecomposite AC-to-DC converters with voltage boosting capability. Moreparticularly, such converters may produce voltage boosting passivelywith an autotransformer that operates with a high ACR. Additionally,phase shifting may occur between power applied to a main rectifier andpower applied to auxiliary rectifiers. Such converters may produce onlyminimal low frequency harmonic distortion of input AC current andvoltage.

Referring now to FIG. 1, it may be seen that an exemplary AC-to-DCconverter 100 may include an autotransformer 120, a main rectifier 140and auxiliary rectifiers 160 and 180, In FIG. 1 the converter 100 isshown interconnected between a 3-phase power supply 200 and a DC load220. The main rectifier 140 and the auxiliary rectifiers 160 and 180 maybe conventional 6 pulse rectifiers.

The autotransformer 120 may be connected to the power supply 200 atprimary terminals 202, 204 and 206. The main rectifier 140 may beconnected to the autotransformer 120 at secondary terminals 142, 144 and146. The auxiliary rectifier 160 may be connected to the autotransformer120 at secondary terminals 162, 164 and 166. The auxiliary rectifier 180may be connected to the autotransformer 120 at secondary terminals 182,184 and 186.

Referring now to FIGS. 2 and 3, detailed illustration ofinterconnections within an exemplary embodiment of the autotransformer120 are shown. The autotransformer 120 may be constructed with threewinding assemblies designated generally as X, Y and Z. The windingassembly X may be wound to include six sequential winding segmentsdesignated XA, XB, XC, XD, XE and XF. The winding assembly Y may bewound include six sequential winding segments designated YA, YB, YC, YD,YE and YF. The winding assembly Z may include six sequential windingsegments designated ZA, ZB, ZC, ZD, ZE and ZF.

Referring particularly to FIG. 3, the winding segment XA may beconnected to the terminal 142 at a point designated X1. The windingsegments XA and XB may be connected together at points X2 and X3. A tap121 may be interposed between the points X2 and X3. The winding segmentsXB and XC may be connected together at points X4 and X5. A tap 122 maybe interposed between the points X4 and X5. The winding segments XC andXD may be connected together at points X6 and X7. A tap 123 may beinterposed between the points X6 and X7

The winding segment YA may be connected to the terminal 144 at a pointdesignated Y1. The winding segments YA and YB may be connected togetherat point Y2 and Y3. A tap 124 may be interposed between the points Y2and Y3. The winding segments YB and YC may be connected together atpoints Y4 and Y5. A tap 125 may be interposed between the points Y4 andY5. The winding segments YC and YD may be connected together at pointsY6 and Y7. A tap 126 may be interposed between the points Y6 and Y7

The winding segment ZA may be connected to the terminal 146 at a pointdesignated Z1. The winding segments ZA and ZB may be connected togetherat point Z2 and Z3. A tap 127 may be interposed between the points Z2and Z3. The winding segments ZB and ZC may be connected together atpoints Z4 and Z5. A tap 128 may be interposed between the points Z4 andZ5. The winding segments ZC and ZD may be connected together at pointsZ6 and Z7. A tap 129 may be interposed between the points Z6 and Z7

The winding assembly X may be interconnected with the winding assembly Ythrough an interconnection between point X8 and the tap 124 and alsothrough an interconnection between a point X9 and the tap 125. Thewinding assembly Y may be interconnected with the winding assembly Zthrough an interconnection between point Y8 and the tap 127 and alsothrough an interconnection between a point Y9 and the tap 128. Thewinding assembly Z may be interconnected with the winding assembly Xthrough an interconnection between point Z8 and the tap 121 and alsothrough an interconnection between a point Z9 and the tap 122.

The winding segment XE may be connected to the secondary terminal 186 ata point X10. In that regard the winding segment XE may be interposedbetween the secondary terminal 186 and winding assembly Y. Similarly,the winding segment YE may be connected to the secondary terminal 184 ata point Y10. In that regard the winding segment YE may be interposedbetween the secondary terminal 186 and winding assembly Z. Also, thewinding segment YE may be connected to the secondary terminal 182 at apoint Y10. In that regard the winding segment YE may be interposedbetween the secondary terminal 182 and winding assembly X.

The winding segment XF may be connected to the secondary terminal 162 ata point X11 and connected to the tap 129 at a point X12. In that regardthe winding segment XF may be interposed between the secondary terminal162 and winding assembly Z. Similarly, the winding segment YF may beconnected to the secondary terminal 166 at a point Y11 and connected tothe tap 123 at a point Y12. In that regard the winding segment YF may beinterposed between the secondary terminal 166 and winding assembly X.Also, the winding segment ZF may be connected to the secondary terminal164 at a point Z10 and connected to the tap 126 at a point Z12. In thatregard the winding segment ZF may be interposed between the secondaryterminal 164 and winding assembly Y.

Referring now particularly to FIG. 2, the various winding assemblies X,Y and Z are shown in a format consistent with a vector analysis point ofview. In that regard a central isosceles triangle 130 may be formed fromsome of the winding segments. A first side 132 of the triangle 130 mayinclude the winding segments XB, XC and XD of the winding assembly X. Asecond side 134 of the triangle 130 may include the winding segments YB,YC and YD of the winding assembly Y. A third side 136 of the trianglemay include the winding segments ZB, ZC and ZD of the winding assemblyZ.

Winding turns ratios of the winding segments may be quantified byconsidering each of the three triangle sides 132, 134 and 136 to have aunit length. In such a normalized context the winding segments may havewinding turns ratios consistent with the following Table 1.

TABLE 1 Winding Segment Turns Ratio XA 0.618 XB 0.1804 XC 0.0959 XD0.7238 XE 0.4660 XF 0.6807 YA 0.618 YB 0.1804 YC 0.0959 YD 0.7238 YE0.4660 YF 0.6807 ZA 0.618 ZB 0.1804 ZC 0.0959 ZD 0.7238 ZE 0.4660 ZF0.6807

In the exemplary embodiment of the converter 100 shown FIG. 1 and theautotransformer of FIGS. 2 and 3, the converter 10 may provide aconverter boost of 1.0:2.0 (input to output) with a W/VA of about 0.711.Prior art converters using a typical isolation transformer present0.5W/VA. This particular W/A improvement indicates a converter probablesize/weight reduction of 29.7%, 1-(0.5/0.711), compared to a prior artboost converter. This improvement may be possible in because of anasymmetric output of this autotransformer. In this configuration, themain rectifier 140 may conduct current for 80 degrees and the twoauxiliary rectifier 160 and 180 may conduct 20 degrees each.

The asymmetrical nature of the converter 100 may be illustrated byconsidering current paths between the AC power supply 200 and therectifiers 140, 160 and 180. It may be seen that a main current path,designated in Table 2 by the numeral 1002, between primary terminal 202and secondary terminal 142 (i.e., a terminal of the main rectifier 140)may have relatively low operational impedance as compared to a firstauxiliary current path, designated in Table 2 by the numeral 1008,between the primary terminal 202 and the secondary terminal 162 (i.e., aterminal of the auxiliary rectifier 160). A second auxiliary currentpath, designated in Table 2 by the numeral 1014, between the primaryterminal 202 and the secondary terminal 184 (i.e., a terminal of theauxiliary rectifier 180) may have a lower operational impedance than themain current path 1002 and an operational impedance different from thefirst auxiliary current path 1008. A Table 2 summarizes the variouscurrent paths that may exist within the autotransformer 120.

TABLE 2 Current path number identity Current path endpoints 1002 Primaryterminal 202 to main secondary terminal 142 1004 Primary terminal 204 tomain secondary terminal 144 1006 Primary terminal 206 to main secondaryterminal 146 1008 Primary terminal 202 to secondary terminal 162 offirst auxiliary rectifier 160 1010 Primary terminal 204 to secondaryterminal 166 of first auxiliary rectifier 160 1012 Primary terminal 206to secondary terminal 164 of first auxiliary rectifier 160 1014 Primaryterminal 202 to secondary terminal 182 of second auxiliary rectifier 1801016 Primary terminal 204 to secondary terminal 186 of second auxiliaryrectifier 180 1018 Primary terminal 206 to secondary terminal 184 ofsecond auxiliary rectifier 180

Referring now to FIG. 4, an exemplary embodiment of an AC to DCconverter 400 with a boost capability of 1.0:2.0 (input to output) isshown. The converter 400 may include an autotransformer 420, a mainrectifier 440 and auxiliary rectifiers 460 and 480, In FIG. 4 theconverter 400 is shown interconnected between a 3-phase power supply 490and a DC load 492. The main rectifier 440 and the auxiliary rectifiers460 and 480 may be conventional 6 pulse rectifiers. Just as theconverter 100 is asymmetrical, the converter 400 is also asymmetrical.

The autotransformer 420 may include winding segment designated 4XA, 4XB,4XC, 4XD, 4XD, 4XE, 4XF, 4YA, 4YB, 4YC, 4YD, 4YD, 4YE, 4YF, 4zA, 4ZB,4ZC, 4ZD, 4ZE, and 4ZF. The winding segments may have turns ratios asshown in the following Table 3.

TABLE 3 Winding Segment Turns Ratio 4XA 0.618 4XB 0.1804 4XC 0.7766 4XD0.0431 4XE 0.4660 4XF 0.6897 4YA 0.618 4YB 0.1804 4YC 0.7766 4YD 0.04314YE 0.4660 4YF 0.6897 4ZA 0.618 4ZB 0.1804 4ZC 0.7766 4ZD 0.0431 4ZE0.4660 4ZF 0.6897

Referring now to FIG. 5, an exemplary embodiment of an AC to DCconverter 500 with a boost capability of 1.0:2.0 (input to output) isshown. The converter 500 may include an autotransformer 520, a mainrectifier 540 and auxiliary rectifiers 560 and 580, In FIG. 5 theconverter 500 is shown interconnected between a 3-phase power supply 590and a DC load 592. The main rectifier 540 and the auxiliary rectifiers560 and 580 may be conventional 6 pulse rectifiers. Just as theconverter 100 is asymmetrical, the converter 500 is also asymmetrical.

The autotransformer 420 may include winding segment designated 5XA, 5XB,5XC, 5XD, 5XD, 5XE, 5XF, 5YA, 5YB, 5YC, 5YD, 5YD, 5YE, 5YF, 5ZA, 5ZB,5ZC, 5ZD, 5ZE, and 5ZF. The winding segments may have turns ratios asshown in the following Table 4.

TABLE 4 Winding Segment Turns Ratio 5XA 0.3324 5XB 0.2856 5XC 0.9569 5XD0.0431 5XE 0.4660 5XF 0.6897 5YA 0.3324 5YB 0.2856 5YC 0.9569 5YD 0.04315YE 0.4660 5YF 0.6897 5ZA 0.3324 5ZB 0.2856 5ZC 0.9569 5ZD 0.0431 5ZE0.4660 5ZF 0.6897

It should be understood, of course, that the foregoing relates toexemplary embodiments of the invention and that modifications may bemade without departing from the spirit and scope of the invention as setforth in the following claims.

We claim:
 1. A multi-phase AC-to-DC converter comprising: a mainrectifier; a first auxiliary rectifier; a second auxiliary rectifier;and an autotransformer coupled with the main rectifier, the firstauxiliary rectifier and the second auxiliary rectifier, theautotransformer including; a first winding assembly including: a primaryterminal coupled with an AC power source, a main secondary terminalcoupled with the main rectifier, a first auxiliary secondary terminalcoupled with the first auxiliary rectifier, and a second auxiliarysecondary terminal coupled with the second auxiliary rectifier, whereinoperational impedance between the primary terminal and the mainsecondary terminal is less than operational impedance between theprimary terminal and either the first auxiliary secondary terminal orthe second auxiliary secondary terminal, and wherein operationalimpedance between the primary terminal and the first auxiliary secondaryterminal is different from operational impedance between the primaryterminal and the second auxiliary secondary terminal; a second windingassembly including, a primary terminal coupled with the AC power source,a main secondary terminal coupled with the main rectifier, a firstauxiliary secondary terminal coupled with the first auxiliary rectifier,and a second auxiliary secondary terminal coupled with the secondauxiliary rectifier, wherein operational impedance between the primaryterminal and the main secondary terminal is less than operationalimpedance between the primary terminal and either the first auxiliarysecondary terminal or the second auxiliary secondary terminal andwherein operational impedance between the primary terminal and the firstauxiliary secondary terminal is different from operational impedancebetween the primary terminal and the second auxiliary secondaryterminal; and a third winding assembly including, a primary terminalcoupled with the AC power source, a main secondary terminal coupled withthe main rectifier, a first auxiliary secondary terminal coupled withthe first auxiliary rectifier, and a second auxiliary secondary terminalcoupled with the second auxiliary rectifier, wherein operationalimpedance between the primary terminal and the main secondary terminalis less than operational impedance between the primary terminal of thethird winding assembly and either the first auxiliary secondary terminalor the second auxiliary secondary terminal and wherein operationalimpedance between the primary terminal and the first auxiliary secondaryterminal is different from operational impedance between the primaryterminal and the second auxiliary secondary terminal.
 2. The converterof claim 1 wherein one or more of the winding assemblies includes sixsequentially-wound winding segments.
 3. The converter of claim 2 whereinone or more of the winding assemblies is provided with at least one taponto which a winding segment from another one of the winding assembliesis coupled.
 4. The converter of claim 2 wherein each one of the windingassemblies is provided with at least two taps onto which winding segmentfrom other ones of the winding assemblies are coupled.
 5. The converterof claim 2 wherein one of the winding segments of the first windingassembly is interposed between one of the auxiliary rectifiers and thesecond winding assembly.
 6. The converter of claim 5 wherein one of thewinding segments of the second winding assembly is interposed betweenone of the auxiliary rectifiers and the first winding assembly, and oneof the winding segments of the third winding assembly is interposedbetween one of the auxiliary rectifiers and the second winding assembly.7. The converter of claim 1 wherein each of the winding assemblies isprovided with a secondary terminal positioned at an end thereof.
 8. Anautotransformer for use in an AC to DC converter comprising: a firstwinding assembly that includes a plurality of winding segments and atleast one tap; a second winding assembly that includes a plurality ofwinding segments and at least one tap; a third winding assembly thatincludes a plurality of winding segments and at least one tap; whereinat least one winding segment of the first winding assembly is connectedto the at least one tap of the second winding assembly, wherein at leastone winding segment of the second winding assembly is connected to theat least one tap of the third winding assembly, and wherein at least onewinding segment of the third winding assembly is connected to the atleast one tap of the first winding assembly.
 9. The autotransformer ofclaim 8, wherein one winding segment of the first winding assembly iscoupled with a second tap of the second winding assembly, wherein onewinding segment of the second winding assembly is coupled with a secondtap of the third winding assembly, and wherein one winding segment ofthe third winding assembly is coupled with a second tap of the firstwinding assembly.
 10. The autotransformer of claim 8, wherein onewinding segment of the third winding assembly is coupled with a secondtap of the second winding assembly, wherein one winding segment of thefirst winding assembly is coupled with a second tap of the third windingassembly, and wherein one winding segment of the second winding assemblyis coupled with a second tap of the first winding assembly.
 11. Theautotransformer of claim 8, wherein one winding segment of the firstwinding assembly is coupled with a second tap of the second windingassembly, wherein one winding segment of the second winding assembly iscoupled with a second tap of the third winding assembly, and wherein onewinding segment of the third winding assembly is coupled with a secondtap of the first winding assembly.
 12. The autotransformer of claim 8,wherein the first winding assembly includes six winding segments beingsequentially wound as a first, a second, a third, a fourth, a fifth anda sixth winding segment. wherein the second, third and fourth windingsegments of the first winding assembly have turns ratios of 0.0959,0.7238, and 0.4660, respectively when a collective length of the second,third and fourth winding segment is normalized to unity, wherein thesecond winding assembly includes six winding segments being sequentiallywound as a first, a second, a third, a fourth, a fifth and a sixthwinding segment. wherein the second, third and fourth winding segmentsof the second winding assembly have turns ratios of 0.0959, 0.7238, and0.4660, respectively when a collective length of the second, third andfourth winding segment is normalized to unity. wherein the third windingassembly includes six winding segments being sequentially wound as afirst, a second, a third, a fourth, a fifth and a sixth winding segment.wherein the second, third and fourth winding segments of the thirdwinding assembly have turns ratios of 0.0959, 0.7238, and 0.4660,respectively when a collective length of the second, third and fourthwinding segment is normalized to unity.
 13. The autotransformer of claim12, wherein the first, the fifth and the sixth winding segments of thefirst winding assembly have turns ratios of 0.618, 0.4660 and 0.6807,respectively, relative to unity, wherein the first, the fifth and thesixth winding segments of the second winding assembly have turns ratiosof 0.618, 0.4660 and 0.6807, respectively, relative to unity, andwherein the first, the fifth and the sixth winding segments of the thirdwinding assembly have turns ratios of 0.618, 0.4660 and 0.6807,respectively, relative to unity.
 14. The autotransformer of claim 8,wherein the first winding assembly includes six winding segments beingsequentially wound as a first, a second, a third, a fourth, a fifth anda sixth winding segment. wherein the second, third and fourth windingsegments of the first winding assembly have turns ratios of 0.1804,0.7766, and 0.0431, respectively when a collective length of the second,third and fourth winding segments is normalized to unity, wherein thesecond winding assembly includes six winding segments being sequentiallywound as a first, a second, a third, a fourth, a fifth and a sixthwinding segment. wherein the second, third and fourth winding segmentsof the second winding assembly have turns ratios of 0.1804, 0.7766, and0.0431,respectively when a collective length of the second, third andfourth winding segment is normalized to unity. wherein the third windingassembly includes six winding segments being sequentially wound as afirst, a second, a third, a fourth, a fifth and a sixth winding segment.wherein the second, third and fourth winding segments of the thirdwinding assembly have turns ratios of 0.1804, 0.7766, and 0.0431,respectively when a collective length of the second, third and fourthwinding segments is normalized to unity.
 15. The autotransformer ofclaim 14, wherein the first, the fifth and the sixth winding segments ofthe first winding assembly have turns ratios of 0.618, 0.4660 and0.6807, respectively, relative to unity, wherein the first, the fifthand the sixth winding segments of the second winding assembly have turnsratios of 0.618, 0.4660 and 0.6807, respectively, relative to unity, andwherein the first, the fifth and the sixth winding segments of the thirdwinding assembly have turns ratios of 0.618, 0.4660 and 0.6807,respectively, relative to unity.
 16. The autotransformer of claim 8,wherein the first winding assembly includes six winding segments beingsequentially wound as a first, a second, a third, a fourth, a fifth anda sixth winding segment. wherein the third and fourth winding segmentsof the first winding assembly have turns ratios of 0.9569 and 0.0431,respectively when a collective length of the third and fourth windingsegments is normalized to unity, wherein the second winding assemblyincludes six winding segments being sequentially wound as a first, asecond, a third, a fourth, a fifth and a sixth winding segment. whereinthe third and fourth winding segments of the second winding assemblyhave turns ratios of 0.9569 and 0.0431, respectively, when a collectivelength of the third and fourth winding segment is normalized to unity.wherein the third winding assembly includes six winding segments beingsequentially wound as a first, a second, a third, a fourth, a fifth anda sixth winding segment. wherein the third and fourth winding segmentsof the third winding assembly have turns ratios of 0.9569 and 0.0431,respectively when a collective length of the third and fourth windingsegments is normalized to unity.
 17. The autotransformer of claim 16,wherein the first, the second, the fifth and the sixth winding segmentsof the first winding assembly have turns ratios of 0.3324, 0.2856,0.4660 and 0.6897, respectively, relative to unity. wherein the first,the second, the fifth and the sixth winding segments of the secondwinding assembly have turns ratios of 0.3324, 0.2856, 0.4660 and 0.6897,respectively, relative to unity, and wherein the first, the second, thefifth and the sixth winding segments of the third winding assembly haveturns ratios of 0.3324, 0.2856, 0.4660 and 0.6897, respectively,relative to unity.